View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 59120U 26145.34802361 +.00000000 +00000-0 +19686-3 0 00008
2 59120 97.5517 293.0883 0006037 287.8398 72.2191 15.44218740 05
| Epoch (UTC): | 25 May 2026 08:21:09 |
| Eccentricity: | 0.0006037 |
| inclination: | 97.5517° |
| perigee height: | 430 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 293.0883° |
| argument of perigee: | 287.8398° |
| revolutions per day: | 15.44218740 |
| mean anomaly at epoch: | 72.2191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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